GEARBOX FOR GAS TURBINE ENGINE

• US 20160230843A1
• Filed: 02/09/2015
• Published: 08/11/2016
• Est. Priority Date: 02/09/2015
• Status: Abandoned Application

• Current Assignee: United Technologies Corporation (Rtx Corporation)
• Original Assignee: United Technologies Corporation (Rtx Corporation)
• Inventors: Duong, Hung, Snape, Nathan
• Application Number:
  US14/617,428
• Publication Number:
  US 20160230843A1
• Time in Patent Office: Days
• US Class Current: 1/1
• CPC Class Codes: F02C 7/32 Arrangement, mounting, or driving, of auxiliaries
• CPC Class Codes: F02K 3/06 with front fan
• CPC Class Codes: F05D 2250/312 the axes being parallel to each other
• CPC Class Codes: F05D 2260/53 using gears
• CPC Class Codes: F16H 1/206 characterised by the driving or driven member being composed of two or more gear wheels
• CPC Class Codes: F16H 1/22 with a plurality of driving or driven shafts; with arrangements for dividing torque between two or more intermediate shafts
• CPC Class Codes: F16H 57/021 Shaft support structures, e.g. partition walls, bearing eyes, casing walls or covers with bearings

Abstract

A gearbox for a gas turbine engine includes a housing that includes a cavity provided between opposing first and second mounting surfaces. An input gear shaft is coupled to a drive gear. The drive gear is connected to first and second shaft portions that respectively extend to the first and second mounting surfaces. The first and second shaft portions and the drive gear are coaxial with one another.

Claims

1. A gearbox for a gas turbine engine comprising:

a housing that includes a cavity provided between opposing first and second mounting surfaces; and

an input gear shaft coupled to a drive gear, the drive gear connected to first and second shaft portions that respectively extend to the first and second mounting surfaces, the first and second shaft portions and the drive gear coaxial with one another.

2. The gearbox according to claim 1, comprising a gear train having multiple drive gears that includes the drive gear, each of the multiple drive gears have first and second shaft portions coaxial with one another and their respective drive gear.

3. The gearbox according to claim 2, wherein the multiple drive gears include first, second and third drive gears, the first drive gear corresponds to the drive gear.

4. The gearbox according to claim 3, wherein the gear train includes an idler gear coupling at least two of the multiple drive gears.

5. The gearbox according to claim 4, wherein the gear train includes first and second idler gears, the first idler gear corresponds to the idler gear, the first and second gears arranged in alternating relationship with the first, second and third drive gears.

6. The gearbox according to claim 2, wherein all of the shaft portions are parallel with one another.

7. The gearbox according to claim 6, wherein the multiple drive gears are in the same plane.

8. The gearbox according to claim 2, comprising accessory drive components that include at least two of an air turbine starter, a deoiler, a variable frequency generator, a permanent magnet alternator, a fuel pump, a lubrication pump and a hydraulic pump, the at least two of the accessory drive components configured to be rotationally driven by the multiple drive gears, one of the at least two of the accessory drive components mounted to the first mounting surface, and the other of the at least two accessory drive components mounted to the second mounting surface.

9. The gearbox according to claim 8, wherein the at least two accessory drive components are the air turbine starter and the deoiler.

10. The gearbox according to claim 8, wherein the at least two accessory drive components are the variable frequency generator and the permanent magnet alternator.

11. The gearbox according to claim 8, wherein the at least two accessory drive components are the fuel pump and the lubrication pump.

12. The gearbox according to claim 1, wherein the input gear shaft is coupled to a gear set that is connected to the drive gear, the gear set includes a bevel gear.

13. The gearbox according to claim 1, wherein the first and second mounting surfaces are parallel to one another.

14. A gas turbine engine comprising:

a core that includes a turbine shaft configured to rotate about an engine axis;

a tower shaft coupled to the turbine shaft;

a gearbox mounted to the core, the gearbox includes;

a housing that includes a cavity provided between opposing first and second mounting surfaces,

an input gear shaft coupled to the tower shaft,

a drive gear connected to first and second shaft portions that respectively extend to the first and second mounting surfaces, the drive gear configured to rotate about a gear axis,

first and second accessory drive components respectively mounted to the first and second mounting surfaces and respectively coupled to the first and second shaft portions.

15. The engine according to claim 14, wherein the engine axis and gear axis are perpendicular to one another.

16. The engine according to claim 14, comprising a gear train having multiple drive gears that includes the drive gear, each of the multiple drive gears have first and second shaft portions coaxial with one another and their respective drive gear, wherein the multiple drive gears include first, second and third drive gears, the first drive gear corresponds to the drive gear.

17. The engine according to claim 16, wherein the gear train includes an idler gear coupling at least two of the multiple drive gears.

18. The engine according to claim 16, wherein all of the shaft portions are parallel with one another, the first and second mounting surfaces are parallel to one another, and the multiple drive gears are in the same plane.

19. The engine according to claim 16, wherein the accessory drive components include at least two of an air turbine starter, a deoiler, a variable frequency generator, a permanent magnet alternator, a fuel pump, a lubrication pump and a hydraulic pump, the at least two of the accessory drive components configured to be rotationally driven by the multiple drive gears, one of the at least two of the accessory drive components mounted to the first mounting surface, and the other of the at least two accessory drive components mounted to the second mounting surface.

20. The engine according to claim 19, wherein the at least two accessory drive components are the air turbine starter and the deoiler.

21. The engine according to claim 19, wherein the at least two accessory drive components are the variable frequency generator and the permanent magnet alternator.

22. The engine according to claim 19, wherein the at least two accessory drive components are the fuel pump and the lubrication pump.